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      비행단계 식별 알고리즘을 이용한 초고속 표적의 탄착점 예측 = Impact Point Prediction of the Ballistic Target Using a Flight Phase Discrimination

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      https://www.riss.kr/link?id=A102114375

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      다국어 초록 (Multilingual Abstract)

      It is required to have the capability to predict the impact point of the ballistic target in order to assign the firing unit with high engagement possibility for the interception in the ballistic target defense systems. In this paper, a novel method is proposed to predict the impact point of the ballistic target using a flight phase discrimination algorithm given the insufficient measurements on the partial trajectory. The flight of a ballistic target is composed of a boost phase and a ballistic phase with different dynamics. The flight phase is discriminated by using the normalized innovation distance between measurements and a priori estimated measurements. The threshold and tolerance in the flight phase discrimination are determined from the probabilistic characteristics of the estimation error. Monte Carlo simulations are performed to verify the proposed method.
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      It is required to have the capability to predict the impact point of the ballistic target in order to assign the firing unit with high engagement possibility for the interception in the ballistic target defense systems. In this paper, a novel method i...

      It is required to have the capability to predict the impact point of the ballistic target in order to assign the firing unit with high engagement possibility for the interception in the ballistic target defense systems. In this paper, a novel method is proposed to predict the impact point of the ballistic target using a flight phase discrimination algorithm given the insufficient measurements on the partial trajectory. The flight of a ballistic target is composed of a boost phase and a ballistic phase with different dynamics. The flight phase is discriminated by using the normalized innovation distance between measurements and a priori estimated measurements. The threshold and tolerance in the flight phase discrimination are determined from the probabilistic characteristics of the estimation error. Monte Carlo simulations are performed to verify the proposed method.

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      참고문헌 (Reference)

      1 권용수, "탄도미사일의 비행궤적 특성 해석" 한국국방경영분석학회 32 (32): 176-187, 2006

      2 이동관, "초고속 표적의 탄도계수와 예상요격지점 정확도의 상관관계 분석 연구" 한국군사과학기술학회 17 (17): 265-274, 2014

      3 J. K. Jung., "The Novel Impact Point Prediction of a Ballistic Target with Interacting Multiple Models" 450-453, 2013

      4 D. K. Ko, "Technology Trend of the Short-range Ballistic Missiles" (335) : 92-101, 2007

      5 P. Zarchan, "Tactical and Strategic Missiles Guidance, Fourth Edition" AIAA Inc. 2002

      6 P. S. Maybeck, "Stochastic Models, Estimation, and Control, Vol. 1" Academic Press 1982

      7 M. S. Grewal, "Kalman Filtering Theory and Practice Using MATLAB, 2nd Edition" John Wiley & Sons, Inc. 2001

      8 T. Yuan., "Impact Point Prediction for Short Range Thrusting Projectiles" 2010

      9 Y. H. Lee, "Flight Trajectory of Ballistic Missiles" 4 (4): 62-77, 1998

      10 Y. Bar-Shalom, "Estimation with Application to Tracking and Navigation : Theory, Algorithm and Software" John Wiley & Sons 2001

      1 권용수, "탄도미사일의 비행궤적 특성 해석" 한국국방경영분석학회 32 (32): 176-187, 2006

      2 이동관, "초고속 표적의 탄도계수와 예상요격지점 정확도의 상관관계 분석 연구" 한국군사과학기술학회 17 (17): 265-274, 2014

      3 J. K. Jung., "The Novel Impact Point Prediction of a Ballistic Target with Interacting Multiple Models" 450-453, 2013

      4 D. K. Ko, "Technology Trend of the Short-range Ballistic Missiles" (335) : 92-101, 2007

      5 P. Zarchan, "Tactical and Strategic Missiles Guidance, Fourth Edition" AIAA Inc. 2002

      6 P. S. Maybeck, "Stochastic Models, Estimation, and Control, Vol. 1" Academic Press 1982

      7 M. S. Grewal, "Kalman Filtering Theory and Practice Using MATLAB, 2nd Edition" John Wiley & Sons, Inc. 2001

      8 T. Yuan., "Impact Point Prediction for Short Range Thrusting Projectiles" 2010

      9 Y. H. Lee, "Flight Trajectory of Ballistic Missiles" 4 (4): 62-77, 1998

      10 Y. Bar-Shalom, "Estimation with Application to Tracking and Navigation : Theory, Algorithm and Software" John Wiley & Sons 2001

      11 문경록, "Comparison of Ballistic-Coefficient-Based Estimation Algorithms for Precise Tracking of a Re-Entry Vehicle and its Impact Point Prediction" 한국우주과학회 29 (29): 363-374, 2012

      12 A. Farina., "Classification and Launch-Impact Point Prediction of Ballistic Target via Multiple Model Maximum Likelihood Estimation(MM-MLE)" 802-806, 2006

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2026 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2017-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2013-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2010-01-01 평가 등재학술지 유지 (등재후보2차) KCI등재
      2007-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2006-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.13 0.13 0.1
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.09 0.09 0.244 0.04
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